|
gptkbp:instanceOf
|
rocket stage
|
|
gptkbp:annualRidership
|
over 30
|
|
gptkbp:chemicalFormula
|
N2O4
|
|
gptkbp:controls
|
digital control system
|
|
gptkbp:developer
|
Fregat-SB
|
|
gptkbp:diameter
|
2.5 meters
|
|
gptkbp:engine
|
1
|
|
gptkbp:engineType
|
liquid rocket engine
|
|
gptkbp:firstFlight
|
2000
2021
|
|
gptkbp:fuelType
|
UDMH
|
|
gptkbp:future_plans
|
geostationary transfer orbit
sun-synchronous orbit
low_Earth_orbit
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Fregat-M
|
|
gptkbp:internationalRelations
|
multiple countries
|
|
gptkbp:is_used_in
|
orbital insertion
|
|
gptkbp:launchDate
|
varies
|
|
gptkbp:launchSite
|
Baikonur Cosmodrome
|
|
gptkbp:launchVehicle
|
gptkb:Soyuz
Proton
Zenit
|
|
gptkbp:length
|
3.7 meters
|
|
gptkbp:manufacturer
|
gptkb:Moscow_Institute_of_Thermal_Technology
|
|
gptkbp:missions
|
gptkb:Gonets-M
gptkb:SES-4
KazSat-3
Intelsat 15
Eutelsat 3B
|
|
gptkbp:notable_feature
|
high precision
high reliability
flexible mission profiles
restartable engine
multiple payload configurations
|
|
gptkbp:offers
|
approximately $10 million
|
|
gptkbp:operates_in
|
gptkb:Arianespace
gptkb:Russian_Space_Forces
|
|
gptkbp:operational_status
|
active
|
|
gptkbp:operationalHistory
|
2000
|
|
gptkbp:passenger_traffic
|
4 meters
1,200 kg
1,500 kg
|
|
gptkbp:payloadCapacity
|
multiple payloads
|
|
gptkbp:propulsion
|
19.6 kN
|
|
gptkbp:provides
|
inertial guidance
|
|
gptkbp:reliability
|
proven
|
|
gptkbp:succeededBy
|
high
|
|
gptkbp:successor
|
Fregat-SB
|
|
gptkbp:weight
|
1,200 kg
|